Recent Investigation of Temperature Recovery and Heat Transmission on Cones and Cylinders in Axial Flow in the N.O.L. Aeroballistics Wind Tunnel
- 1 January 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (1), 1-6
- https://doi.org/10.2514/8.2139
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- The Transient Temperature Distribution in a Wing Flying at Supersonic SpeedsJournal of the Aeronautical Sciences, 1950